Path: Orbit/Optimization
% Demonstrate the 2D trajectory optimization function for low thrust. This demo is the same as the built-in demo in TrajectoryOptimization, a low-thrust transfer to Mars. This is a well-studied problem. The method used is downhill simplex. Things to try: see how the methods do with different initial costates. See also Constant, Planets, TrajectoryOptimization %
Orbit: Optimization/CostLowThrust2D Orbit: Optimization/FLowThrust2D Orbit: Optimization/Plot2DTrajectory Orbit: Optimization/TrajectoryOptimization SC: BasicOrbit/VOrbit SC: Ephem/Planets Common: Database/Constant
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